搜索资源列表
InertialMeasurement
- 惯性导航C语言程序,比例方程解算C语言程序，用四元数法更新姿态矩阵。-C language program of the inertial navigation, the proportion of equation solver C language program to update the attitude matrix, using the quaternion method.
191208pttj9oofqzoj63go
- 四元数算法微四轴姿态解算源码。拿出来和大家一起分享。-Quaternion algorithm source micro-axis attitude solution. Out and share with everyone.
SOFT_DESIGN
- 本设计是基于STM32F4的四轴航拍平台。以STM32F407为控制核心，四轴飞行器为载体，辅以云台的航拍系统。硬件上由飞控电路，电源管理，通信模块，动力系统，机架，云台伺服系统组成。算法上采用简洁稳定的四元数加互补滤波作为姿态解算算法，PID作为控制器，实现飞行，云台增稳等功能。具有灵活轻盈，延展性，适应性强好等特点。-The design is based on a four-axis STM32F4 aerial platform. In STM32F407 as the control
attitude_estimator_q
- Pixhawk飞控基于四元数的姿态解算源码，方法简单有效-Pixhawk flight control based on quaternion attitude algorithm source code, the method is simple and effective
flycontrol
- 四轴飞行器飞控程序，串级PID，外环PI内环PID，四元数互补滤波，辅助三角函数姿态解算。-Four-axis aircraft flight control procedures, Cascade PID, PI outer inner PID, quaternion complementary filter, auxiliary trigonometric attitude solution.
MPU6050姿态解算
- STM32对MPU6050的四元数姿态解算，
Myfly_IMU6050_ZI_250_dinggao
- 本人做的四轴飞行器，可以平稳飞行，可平稳定高飞行，内含mpu6050，5883l，气压计，超声波驱动，四元数姿态解算，串行PID控制姿态和定高。-I do four-axis aircraft, a smooth flight, can fly high level of stability, containing mpu6050,5883l, barometer, ultrasound drive, quaternion attitude algorithm, serial PID contr
Myfly_IMU6050_ZI_250_yaokong
- 本人做的四旋翼飞行器源码，这个是纯遥控版，可以实现稳定飞行，内含mpu6050,5883l，等传感器驱动，以及四元数姿态解算，和PID，以及遥控的解锁上锁等-I do four rotorcraft source, this is a pure version of the remote control, you can achieve a stable flight, containing mpu6050,5883l, and other sensor-driven, and quaterni
AHRS-DATA
- 基于惯性传感器的姿态解算，输出四元数和欧拉角，常用于惯性导航。-Based on the attitude of the inertial sensor, the output of four elements and Euler angles, commonly used in inertial navigation.
minicraft
- 自己写的四轴飞行器控制程序，包括姿态检测，四元数解算，电机控制，遥控-code for four rotor
08.-MPU6050
- 四元数姿态解算的程序，自己本科时候的毕业设计就是这个。-attitude caculate
四旋翼源代码
- 基于STM32F4的四轴航拍平台。以STM32F407为控制核心，四轴飞行器为载体，辅以云台的航拍系统。硬件上由飞控电路，电源管理，通信模块，动力系统，机架，云台伺服系统组成。算法上采用简洁稳定的四元数加互补滤波作为姿态解算算法，PID作为控制器，实现飞行，云台增稳等功能(Four axis aerial platform based on STM32F4. Taking STM32F407 as the control core, the four axis flying vehicle as
四元数和欧拉角
- 关于四元数和欧拉角的一些资料，挺丰富的，共享一下，希望对大家有帮助。(About four yuan and Euler angle of some information, very rich, share it, I hope all of you help.)
motion_driver-5.1.2
- InvenSense陀螺仪姿态解算，直接输出四元数，省去姿态融合算法的编写，适用于飞控(The attitude calculation of InvenSense gyroscope outputs four elements directly, and avoids the compilation of attitude fusion algorithm, which is suitable for flight control)
imu
- 四元数姿态解算互补滤波无人机IMU 可用于要求精度不高于0.5的无人机使用(The updating attitude algorithm using gyroscope was studied both in theory and execution of computer operation, and then, the quaternion theory based on Runge-Kutta method was choose.)
四元数AHRS姿态解算和IMU姿态解算分析
- 四元数AHRS姿态解算和IMU姿态解算分析(Four element number AHRS attitude calculation and IMU attitude calculation analysis)
基于STM32F4的四轴航拍飞行器
- 本设计是基于STM32F4的四轴航拍平台。以STM32F407为控制核心，四轴飞行器为载体，辅以云台的航拍系统。硬件上由飞控电路，电源管理，通信模块，动力系统，机架，云台伺服系统组成。算法上采用简洁稳定的四元数加互补滤波作为姿态解算算法，PID作为控制器，实现飞行，云台增稳等功能。具有灵活轻盈，延展性，适应性强好等特点。(This design is based on STM32F4's four axis aerial platform. Taking STM32F407 as the con
EKF
- 使用扩展卡尔曼滤波进行姿态解算，输出四元数，可进行参数调节(Use extended Kalman filter for attitude calculation, output quaternion, parameter adjustment)
基于STM32F1的 MPU6500四元数姿态解算代码
- 单片机采用STM32F103，SPI通信方式，通过四元数解算直接获得欧拉角。姿态角稳定。
MPU6500研发代码(四元数)
- 基于STM32F103单片机解算出MPU6500 陀螺仪姿态数据，SPI通信协议，并且CAN总线输出。(Based on STM32F103, the attitude data of mpu6500 gyroscope, SPI communication protocol and can bus output are calculated.)